RESEARCH ON ROTATING STALL IN AXIAL FLOW COMPRESSORS PART Ⅲ. Experiments on Laminar Separation From a Moving Wall

摘要

An experimental program is described which investigates the laminar boundary layer near separation when the wall and separation point are in relative motion. The modal used in the investigation was a two-dimensional rotating cylinder which was tested without and with shrouds to impose an airfoil-type pressure gradient. Limited qualitative data are presented which indicate that there is a relatively large displacement of the separa¬tion point when the wall and separation point are in relative motion. These data qualitatively substantiate the analysis presented as Bart II of the present report.